Hidden nonlinear oscillations in aircraft stabilization system with restrictions at the actuator control

Результат исследований: Публикации в книгах, отчётах, сборниках, трудах конференцийстатья в сборнике материалов конференциинаучнаярецензирование

2 Цитирования (Scopus)

Выдержка

In the paper, the control problem with limitations on the magnitude and rate of the control action in aircraft control systems, is studied. Existence of hidden limit cycle oscillations in the case of actuator position and rate limitations is demonstrated by the examples of piloted aircraft PIO phenomenon and the airfoil flutter suppression system.

Язык оригиналаанглийский
Название основной публикацииICNPAA 2018 World Congress
Подзаголовок основной публикации12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences
РедакторыSeenith Sivasundaram
ИздательAmerican Institute of Physics
Том2046
ISBN (электронное издание)9780735417724
DOI
СостояниеОпубликовано - 4 дек 2018
Событие12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences, ICNPAA 2018 - Yerevan, Армения
Продолжительность: 3 июл 20186 июл 2018

Конференция

Конференция12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences, ICNPAA 2018
СтранаАрмения
ГородYerevan
Период3/07/186/07/18

Отпечаток

aircraft
constrictions
stabilization
actuators
oscillations
aircraft control
flutter
airfoils
retarding
cycles

Предметные области Scopus

  • Физика и астрономия (все)

Цитировать

Andrievsky, B., Kudryashova, E. V., Kuznetsov, N. V., Kuznetsova, O. A., & Mokaev, T. N. (2018). Hidden nonlinear oscillations in aircraft stabilization system with restrictions at the actuator control. В S. Sivasundaram (Ред.), ICNPAA 2018 World Congress: 12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences (Том 2046). [020004] American Institute of Physics. https://doi.org/10.1063/1.5081524
Andrievsky, Boris ; Kudryashova, Elena V. ; Kuznetsov, Nikolay V. ; Kuznetsova, Olga A. ; Mokaev, Timur N. / Hidden nonlinear oscillations in aircraft stabilization system with restrictions at the actuator control. ICNPAA 2018 World Congress: 12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences. редактор / Seenith Sivasundaram. Том 2046 American Institute of Physics, 2018.
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title = "Hidden nonlinear oscillations in aircraft stabilization system with restrictions at the actuator control",
abstract = "In the paper, the control problem with limitations on the magnitude and rate of the control action in aircraft control systems, is studied. Existence of hidden limit cycle oscillations in the case of actuator position and rate limitations is demonstrated by the examples of piloted aircraft PIO phenomenon and the airfoil flutter suppression system.",
author = "Boris Andrievsky and Kudryashova, {Elena V.} and Kuznetsov, {Nikolay V.} and Kuznetsova, {Olga A.} and Mokaev, {Timur N.}",
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editor = "Seenith Sivasundaram",
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Andrievsky, B, Kudryashova, EV, Kuznetsov, NV, Kuznetsova, OA & Mokaev, TN 2018, Hidden nonlinear oscillations in aircraft stabilization system with restrictions at the actuator control. в S Sivasundaram (ред.), ICNPAA 2018 World Congress: 12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences. том. 2046, 020004, American Institute of Physics, Yerevan, Армения, 3/07/18. https://doi.org/10.1063/1.5081524

Hidden nonlinear oscillations in aircraft stabilization system with restrictions at the actuator control. / Andrievsky, Boris; Kudryashova, Elena V.; Kuznetsov, Nikolay V.; Kuznetsova, Olga A.; Mokaev, Timur N.

ICNPAA 2018 World Congress: 12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences. ред. / Seenith Sivasundaram. Том 2046 American Institute of Physics, 2018. 020004.

Результат исследований: Публикации в книгах, отчётах, сборниках, трудах конференцийстатья в сборнике материалов конференциинаучнаярецензирование

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Andrievsky B, Kudryashova EV, Kuznetsov NV, Kuznetsova OA, Mokaev TN. Hidden nonlinear oscillations in aircraft stabilization system with restrictions at the actuator control. В Sivasundaram S, редактор, ICNPAA 2018 World Congress: 12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences. Том 2046. American Institute of Physics. 2018. 020004 https://doi.org/10.1063/1.5081524